session 4
- Title
Guidance, Navigation & Control (2)
- type
oral
- Description
The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft and rockets, including formation flying, rendezvous and docking.
- Date
2017-09-27
- Time
- Room
- IPC members
Co-Chair: Dr. Anton de Ruiter, Ryerson University, Canada;
Co-Chair: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;
Rapporteur: Prof. Igor V. Belokonov, Samara National Research University (Samara University), Russian Federation;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | Stabilization of Underactuated Spacecraft with Two CMGs using Model Predictive Control | 15 | withdrawn | Dr. Haichao Gui | Ryerson University | Canada | |
2 | 15 | confirmed | Mr. Jeffrey Stuart | Jet Propulsion Laboratory - California Institute of Technology | United States | ||
3 | Parallel Spacecraft Solar and Thermal Radiation Pressure Modeling Using Graphic Processing Unit | 15 | confirmed | Mr. Patrick Kenneally | The University of Colorado | United States | |
4 | Ascent Flight Control of Launch Vehicle Using Angle of Attack Estimator | 15 | withdrawn | Mr. Ario Birmiawan Widyoutomo | The Graduate Universty for Advanced Studies (SOKENDAI) | Japan | |
5 | Docking of a space tug with upper stage debris object using deployable flexible beam | 15 | confirmed | Prof. Vladimir S. Aslanov | Samara National Research University (Samara University) | Russian Federation | |
6 | a paper and pencil method of evaluating trajectories of space launchers | 15 | confirmed | Prof. Paolo Teofilatto | Sapienza - University of Rome | Italy | |
7 | 15 | confirmed | Dr. ZHIYONG SHE | Beijing Aerospace Technology Institute | China | ||
8 | New Implicit Neighboring Optimal Guidance and Attitude Control for Three-dimensional Lunar Ascent | 15 | confirmed | Dr. Mauro Pontani | Sapienza - University of Rome | Italy | |
9 | Tether length control in tether-assisted deorbiting mission from an elliptical orbit | 15 | confirmed | Prof. Vladimir S. Aslanov | Samara National Research University (Samara University) | Russian Federation | |
10 | magneto-coulombic fault tolerant sliding mode attitude control of earth pointing satellites | 15 | confirmed | Mr. Himanshu Prabhat | IIT Kharagpur | India | |
11 | Orientation Optimisation of a Four Reaction Wheel Satellite Control System for Fault Tolerance | 15 | confirmed | Dr. Zebb Prime | Australia | ||
12 | Launch Vehicle Adaptive Flight Control with Incremental Model Based Heuristic Dynamic Programming | 15 | confirmed | Ms. Ye Zhou | Delft University of Technology (TU Delft) | The Netherlands |